
FMS-D212-725-1
Page 2-11
• COPYRIGHT © 2007 BY DART AEROSPACE LTD •
This document is private and confidential and is supplied on the express condition that it is not to be used for any
purpose or copied or communicated to any other person without written permission from Dart Aerospace Ltd.
Revision:
G
TC Approved Date: 13.08.09
2
nd
tail rotor driveshaft – Check.
Heater compartment – Check heater for condition and security. Area clear of
obstructions. Secure door.
Engine oil level – Verify presence of oil in sight gauge and proper oil level.
Engine compartment – Check fuel and oil lines and connections for condition,
security and leaks. Check fluid levels. Secure cowling.
Fuel filler – Visually check quantity; secure cap.
9. AREA 9 – FUSELAGE RIGHT SIDE
Fuselage – Check condition of skin.
Passenger door – Check condition and operation; glass clean. Condition and
security of pop-out windows.
Transmission oil level – Check.
Right Hydraulic Reservoir – Visually check fluid level
Landing gear – Condition; handling wheels removed.
Navigation and position lights – Security and condition.
10. AREA 10 – CABIN TOP
Warning
SNOW AND ICE SHALL BE REMOVED PRIOR TO
FLIGHT WHEN HELICOPTER HAS BEEN EXPOSED
TO SNOW AND ICING CONDITIONS.
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